19991007036939A

(.19) On October 7, 1999, at 1015 hours mountain standard time, a Bell 206B, N6624N, experienced a loss of engine power and force landed in Apache Junction, Arizona. The helicopter, operated by Bell ford, inc., of phoenix, Arizona, sustained substantial damage. The commercial pilot and two passengers were not injured. The local personal flight, conducted under the provisions of 14 CFR part 91, originated from falcon field, mesa, Arizona, about 1000. Visual meteorological conditions prevailed and no flight plan was filed. The pilot reported that he experienced a complete loss of engine power and performed an autorotation. The main rotor blades severed the tail boom. The engine was examined and it was noted that the nos. 6 and 7 bearings had failed. This accident was not reported to the safety board until December 20, 1999. (-23)pilot was in cruise flight, approx. 600 ft. (AGL) when engine oil pressure indicated very high ("red-line"), torque went to max. On instrument, and the engine oil "chip" light illuminated-all simultaneously. The pilot entered an autorotative descent and contacted the ground at approx. 20 mph (indicated ground speed). The forward portion of the l/h landing, skid contacted a creosote bush and the helicopter scewed left, tail high coming to rest after a low n caused the main rotor blades to contact the tail boom aft of the horz. Stabilizer. No injuries , no fire. (.4)on October 7, 1999, at 1015 hours mountain standard time, a Bell 206B, N6624N, experienced a loss of engine power and collided with high vegitation during a forced landing near Apache Junction, Arizona. The helicopter, operated by Arizona heliservices, inc., of chandler, Arizona, sustained substantial damage. The commercial pilot and two passengers were not injured. The local personal flight, conducted under the provisions of 14 CFR part 91, originated from the cochise county airport, willcox, Arizona, about 0905, and was en route to falcon field, mesa, Arizona. Visual meteorological conditions prevailed and no flight plan was filed. The pilot reported that while in cruise flight about 600 feet AGL, he noticed that the engine oil pressure was "exceedingly high," and the torque gauge was exceeding the high limits (120+). The engine chip light became illuminated. The pilot lowered the collective with no apparent effect on the torque gauge reading. As he descended to make an immediate landing, the engine quit about 75 to 100 feet AGL. The pilot autorotated to the ground with a slight aft skid touchdown and minimum forward airspeed. The left skid toe became embedded in a creosote bush and the helicopter turned left 90 degrees. The left skid separated from the crossmember and the left side of the nose dipped. The main rotor blades severed the tail cone aft of the horizontal stabilizer. The right skid separated but the helicopter remained upright. A teardown examination of the engine was conducted. The mechanic reported that the nos. 6 and 7 bearings displayed evidence of heat distress and oil starvation. He blew through the oil jet for the nos. 6 and 7 bearings and thought it seemed to be partially blocked. He then blew compressed air through the oil jet and heard something pop out. He opined that it might have been a piece of carbon, which could have clogged the jet and blocked the flow of oil. He stated that all other components of the lubrication system were intact and functional. No other discrepancies were found.